Patent US3788267A successfully refreshed from Google Patents.
US3788267A
Expired / Lapsed
US
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Anti-cavitation means for marine propulsion device
Assignee: Brunswick Corp
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Filing: 1971-12-17
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Granted: 1974-01-29
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Expires: 1991-12-17
Abstract
Abstract Cavitation eminating from the leading edge near the hub of a propeller of a marine propulsion device is prevented by introducing exhaust gas air adjacent the junction of the leading edge of each blade of the propeller and the propeller hub from the interior of the hub through which the exhaust gas or air flows.
Inventors
- 👤 W Strong
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 15:08
CPC Classifications
B; B63; B63H; B63H20/00; B63H20/24; B63H20/26; B63H1/00; B63H1/02; B63H1/12; B63H1/14; B63H1/18
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
163 words
In a marine propulsion device having an outboard drive unit with an internal chamber in communication with a source of gas, a rotatable propeller carried by said drive unit and having an inner hub, an outer bub spaced therefrom to define a primary annular passage therethrough in communication with said chamber to pass substantially all of said gas from said chamber out the rear of the propeller, and at least two blades extending radially outwardly from said outer hub forward of said propeller rear; the improvement comprising secondary passage means to provide communication from said passage to an area adjacent the face of each of said blades to release a minor amount of said gas from said passage along the root of each of said blades such that any vacuum therealong is relieved, said secondary passaGe means including at least one aperture in said outer bhub associated with each propeller blade, said aperture being positioned adjacent to the face of its associated blade.
Claim 2
Dependent Claim
163 words
In a marine propulsion device having an outboard drive unit with an internal chamber in communication with a source of gas, a rotatable propeller carried by said drive unit and having an inner hub, an outer bub spaced therefrom to define a primary annular passage therethrough in communication with said chamber to pass substantially all of said gas from said chamber out the rear of the propeller, and at least two blades extending radially outwardly from said outer hub forward of said propeller rear; the improvement comprising secondary passage means to provide communication from said passage to an area adjacent the face of each of said blades to release a minor amount of said gas from said passage along the root of each of said blades such that any vacuum therealong is relieved, said secondary passaGe means including at least one aperture in said outer bhub associated with each propeller blade, said aperture being positioned adjacent to the face of its associated blade.
Claim 3
Dependent Claim
22 words
The improvement according to claim 1 in which said second passages extend substantially perpendicular to the axis of rotation of said propeller.
Claim 4
Dependent Claim
19 words
The improvement according to claim 2 in which the source of gas is the exhaust of the propulsion device.
Claim 5
Dependent Claim
31 words
The improvement according to claim 2 in which each of said second passages is disposed adjacent the junction of the leading edge of one of said blades and said outer hub.
Claim 6
Dependent Claim
63 words
The improvement according to claim 1 in which said secondary passage means includes a plurality of passages for each of said blades extending through said outer hub from said primary annular passage to the exterior of said outer hub and said passages for each of said blades being longitudinally spaced from each other in the direction of the rotational axis of said propeller.
Claim 7
Dependent Claim
24 words
The improvement according to claim 5 in which each of said second passages extends substantially perpendicular to the axis of rotation of said propeller.
Claim 8
Dependent Claim
19 words
The improvement according to claim 1 in which the source of gas is the exhaust of the propulsion device.
References Cited (Backward Citations)
US2213609A
Cited
US3587510A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1977-01-28 | 1977-07-30 | 1978-01-29 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1981-01-28 | 1981-07-30 | 1982-01-29 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1985-01-28 | 1985-07-30 | 1986-01-29 | $7700.00 | Window Closed / Lapsed |